Maximum Takeoff Thrust
334.6798 kN
Overall Pressure Ratio
46.0013
Fuel Flow Take Off
2.5562 kg/s
NOx Unitaryto CAEP8
83.011 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
No |
Gear
—
|
Reduction Ratio
—
|
| LP compressor |
Low-Pressure Compressor Stages
—
|
Low-Pressure Compressor Technology
—
|
BP Compressor Pressure Ratio
—
|
| IP compressor |
Intermediary-Pressure Compressor Stages
—
|
Intermediary-Pressure Compressor Technology
—
|
IP Compressor Pressure Ratio
—
|
| HP compressor |
High-Pressure Compressor Stages
—
|
High-Pressure Compressor Technology
—
|
HP Compressor Pressure Ratio
—
|
| Combustor |
Combustion Chamber
Phase5 Tiled |
| HP turbine |
High Pressure Compressor Stages
—
|
High-Pressure Turbine Technology
—
|
| IP turbine |
Intermediary-Pressure Turbine Stages
—
|
Intermediary-Pressure Turbine Technology
—
|
| LP turbine |
Low-Pressure Turbine Stages
—
|
Low-Pressure Turbine Technology
—
|
| Whole engine |
Streams
2 |
Bypass Ratio
9.0165 |
Overall Pressure Ratio
46.0013 |
Afterburner
No |
Pictures
No pictures yet for this family.
Similar reaction turbines
All data (82 fields)
- Name
- Trent 1000-CE3
- EASA ID
- 02P23RR127
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 9.0165
- Overall Pressure Ratio
- 46.0013
- Maximum Takeoff Thrust (kN)
- 334.6798
- Hydrocarbon Take Off (g/kg fuel)
- 0
- Hydrocarbon Climb Out (g/kg fuel)
- 0
- Hydrocarbon Approach (g/kg fuel)
- 0
- Hydrocarbon Idle (g/kg fuel)
- 0
- Hydrocarbon Unitary Average (g/kN)
- 0
- Hydrocarbon Unitary Sigma (g/kN)
- 0
- Hydrocarbon Unitary Range (g/kN)
- 0-0
- Hydrocarbon Unitary Characteristic (g/kN)
- 0
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 0
- Hydrocarbon LTO (g)
- 0
- Carbon Monoxide Take Off (g/kg fuel)
- 0.4206
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.4249
- Carbon Monoxide Approach (g/kg fuel)
- 0.6086
- Carbon Monoxide Idle (g/kg fuel)
- 6.5128
- Carbon Monoxide Unitary Average (g/kN)
- 8.5461
- Carbon Monoxide Unitary SD (g/kN)
- 1.6565
- Carbon Monoxide Unitary Range (g/kN)
- 5.47-10.65
- Carbon Monoxide Unitary Characteristic (g/kN)
- 8.96
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 7.6
- NOx Take Off (g/kg fuel)
- 55.2833
- NOx Climb Out (g/kg fuel)
- 41.4624
- NOx Approach (g/kg fuel)
- 14.2612
- NOx Idle (g/kg fuel)
- 5.7912
- NOx Unitary Average (g/kN)
- 65.8394
- NOx Unitary SD (g/kN)
- 0.8021
- NOx Unitary Range (g/kN)
- 64.73-66.95
- NOx Unitary Characteristic (g/kN)
- 68.1709
- NOx Unitaryto Standard (% of limit)
- 51.6435
- NOx Unitaryto CAEP2 (% of limit)
- 64.5544
- NOx Unitaryto CAEP4 (% of limit)
- 68.8576
- NOx Unitaryto CAEP6 (% of limit)
- 74.9438
- NOx Unitaryto CAEP8 (% of limit)
- 83.011
- NOx LTO (g)
- 22034.03
- Smoke Take Off (SN)
- 8.2216
- Smoke Climb Out (SN)
- 11.365
- Smoke Approach (SN)
- 9.2631
- Smoke Idle (SN)
- 1.9015
- Smoke Max (SN)
- 14.7
- Smoke Sigma (SN)
- 2
- Smoke Range (SN)
- 11.4-16.7
- Smoke Characteristic (SN)
- 16.4
- Smoke Characteristicto Regulatory (% of limit)
- 96.4
- Fuel Flow Take Off (kg/s)
- 2.5562
- Fuel Flow Climbout (kg/s)
- 2.0896
- Fuel Flow Approach (kg/s)
- 0.6874
- Fuel Flow Idle (kg/s)
- 0.2556
- Fuel LTO (kg)
- 946.9587
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2860.061
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 76.5156
- nvPME Imass Climb Out (mg/kg)
- 76.3119
- nvPME Imass Idle (mg/kg)
- 19.1381
- nvPME Imass Max (mg/kg)
- 152.9596
- nvPME Imass Take Off (mg/kg)
- 44.8013
- nvPME Inum Approach (#/kg)
- 867903500000000
- nvPME Inum Climb Out (#/kg)
- 252640300000000
- nvPME Inum Idle (#/kg)
- 458565400000000
- nvPME Inum Max (#/kg)
- 928140000000000
- nvPME Inum Take Off (#/kg)
- 130296000000000
- nvPMLTO Mass (mg)
- 46114.04
- nvPMLTO Mass Per Thrust (mg/kN)
- 191.5284
- nvPMLTO Mass To CAEP11 (% of limit)
- 89.4993
- nvPMLTO Number (#)
- 409726800000000000
- nvPMLTO Number Per Thrust (#/kN)
- 1701745000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 61.2139
- nvPM Mass Concentration Characteristic (mg/m³)
- 3409.81
- nvPM Mass Concentration Max (mg/m³)
- 2649.081
- nvPM Mass Concentration To CAEP10 (% of limit)
- 87.7011